Optimization of heat transfer on thermal barrier coated gas turbine blade

• Main Authors: Aabid, Abdul, Khan, Sher Afghan
• Format: Conference or Workshop Item
• Language: English; English
• Published: Institute of Physics Publishing 2018
• Subjects: TA401 Materials of engineering and construction; TJ Mechanical engineering and machinery
• Online Access: http://irep.iium.edu.my/65970/1/65970_Optimization%20of%20Heat%20Transfer%20on%20Thermal%20Barrier_conference%20article.pdf; http://irep.iium.edu.my/65970/2/65970_Optimization%20of%20Heat%20Transfer%20on%20Thermal%20Barrier_scopus.pdf; http://irep.iium.edu.my/65970/; http://iopscience.iop.org/article/10.1088/1757-899X/370/1/012022/meta

In the field of Aerospace Propulsion technology, material required to resist the maximum temperature. In this paper, using thermal barrier coatings (TBCs) method in gas turbine blade is used to protect hot section component from high-temperature effect to extend the service life and reduce the ma...